Boeing 717-200
Service difficulty reports · 18,771
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '717200' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '717200' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2017040302634Frame · crackedAFT ACCESORIES BAY, CRACKED FRAME ANGLE BS 1144 BETWEEN LONGERONS 2 - 3L. THE ANGLE WAS REPLACED IAW SRM 51-41-05 AND DWG 9911840, REV CR.SDR DALA2017040302633Pan · crackedCRACK ON UPPER CORNER FWD EDGE INNER PAN AT THE FWD CARGO DOOR. THE PAN WAS REPAIRED IAW SRM 52-30-02-2R, PROCEDURE 1, REPAIR 1.SDR DALA2017040202707Access Panel · corrodedCORROSION ON FUEL ACCES PANEL 520CT. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01.SDR DALA2017040202632Access Panel · corrodedCORROSION ON FUEL TANK ACCESS PANELS 520GB AND 520DT. THE FUEL ACCESS PANEL WERE REPLACED PER B717 SRM 57-10-01. (LP #2956805)SDR DALA2017040202631Frame · crackedCRACKED FRAME BS 706, LONGERONS 25 - 28R. FRAME REPAIRED IAW SRM 51-70-11-2R, REP 1.SDR DALA2017040202630Frame · crackedCRACKED FRAME BS 660, LONGERONS 25 - 28L. THE FRAME WAS REPLACED IAW SRM 51-41-05, AND SRM 51-41-02.SDR DALA2017040202629Beam · crackedCRACKED AFT EDGE OF THE NR 1 BEAM AT THE MAIN ENTRANCE DOOR. THE BEAM WAS REPAIRED IAW SRM 52-10-02-2R, PROCEDURE 7, REPAIR 7 FIG 201.SDR DALA2017040202628Pan · crackedCRACKED PAN ON AFT EDGE NR 1 BEAM AT MAIN ENTRANCE DOOR. THE PAN WAS REPLACED IAW SRM 51-41-01, 51-41-02, 51-41-04, AND 51-41-05.SDR DALA2017040402712Skin · crackedSKIN CRACK ON THE TOP OF THE FUSELAGE AT BS 1133 TO THE LEFT OF THE VERTICAL STAB. REPAIRED THE SKIN IAW ERA 555586-14AD REV 0.SDR DALA2017040402711Skin · crackedSKIN CRACK ON THE TOP OF THE FUSELAGE AT BS 1133 ON THE RIGHT SIDE OF THE VERTICAL STAB. REPAIRED THE SKIN IAW ERA 555587-14AD, REV O.SDR DALA2017040102627Panel · damagedLEFT WING LEADING EDGE AT INBD END NR 3 SLAT HAS THREE LOOSE RIVETS AND LEADING EDGE SPLICE DOUBLER CRACKED. FABRICATED A SPLICE IAW DRAWING 9919376. INSTALLED THE NEW SPLICE IAW DRAWING #9919376.SDR DALA2017040102626Frame · crackedCRACKED FRAME ANGLE BS 1022, LONGERONS 13 - 14L. REPLACED IAW SRM 51-41-02, DWG 9912243, REV JS, AND REPAIRED IAW SRM 53-00-06-2R.SDR DALA2017040102625Door Frame · crackedCRACKS ON NLG DOOR FRAME LT AND RT BS 45. THE DOOR FRAMES WERE REPAIRED IAW SRM 53-10-14, REP 2, FIG 201.SDR DALA2017040102624Door Frame · crackedCRACKED DOOR FRAME WEB BS 207, LONGERON 15L. . REPAIRED IAW SRM 53-10-15-2R-1.SDR DALA2017040502745Floor Support · crackedFORWARD CARGO STA 636, BL0 AFT ANGLE ON INTERCOSTAL IS CRACKED. REPAIRED CRACKED FLOOR SUPPORT "INTERCOSTAL" AT STA 636 BL0 IAW SRM 51-70-11-2R-1.SDR DALA2017033002581Floor Panel · delaminatedDELAMINATION FLOOR PANEL 211 ANF AT COCKPIT. SN 00403 FLOOR PANEL 211 ANF AT COCKPIT WAS FABRICATED AND REPLACED PER SRM 53-20-50.SDR 2017F00048Spoiler · delaminatedDURING UNSCHEDULED MAINTENANCE CHECK RT I/B SPOILER FOUND DELAMINATED.SDR DALA2017040402714Pan · corrodedFWD CARGO DOOR FRAME CORRODED IN SEVERAL PLACES. REPAIRED CARGO FRAME PAN IAW SRM 53-20-15-2R.SDR DALA2017040402713Skin · corrodedLARGE AREA OF BLOW OUT CORROSION BS 737 TO SLANT PANEL LBL 4. REPAIRED THE AREA IAW ERA 555592-14 REV 0.SDR DALA2017032902563Battery Pack · inoperativeEMERGENCY LIGHTS AT SEAT ROWS 20B AND 20CD ARE INOPERATIVE. REPLACED THE BATTERY PACK IAW MM 33-51. LIGHTS OPS NORMAL.SDR DALA2017033002561Access Panel · damagedELONGATED HOLES ON FUEL TANK ACCESS PANEL 520CB. REPAIRED THE ACCESS PANEL IAW SRM 57-10-01-2R-2, PAR. 5 B. (3).SDR DALA2017033002560Access Panel · damagedELONGATED HOLES ON FUEL TANK ACCESS PANEL 520LB. REPAIRED THE ACCESS PANEL IAW SRM 57-10-01-2R-2 PAR. 5 B. (3).SDR DALA2017033002559Structure · crackedFWD CARGO DOOR, A CRACK WAS FOUND ON THE FWD EDGE BETWEEN BEAMS 1 AND 2. REPAIRED IAW SRM 52-30-02-2R-4, FIG 201.SDR SWAA201703290082Skin · delaminatedDURING AN UNSCHEDULE MAINTENANCE CHECK, LT INBD SPOILER FOUND DELAMINATED.SDR DALA2017033002562Cusp Web · puncturedPUNCTURE IN LEFT OTBD CUSP WEB BS 298. REPAIRED THE CUSP WEB IAW SRM 53-00-55-2R-4.SDR DALA2017032902557Floor Support · corrodedCORROSION ON FLOOR SUPPORT FROM BS 161 - 198, RBL 44 IN THE PAX CABIN. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-04, PAR 26, 51-41-02, AND 51-41-05.SDR HALA2017032800088Pitot Head · obstructedAIR TURN BACK FOR MULTIPLE ALERTS BEING DISPLAYED, STICK PUSHER FAIL, A/P NOT AVAILABLE, IAS ANOMALY BETWEEN CAPTAIN & FIRST OFFICER, RUDDER LIMITER FAIL. FOUND BEE LODGED IN CAPTAIN`S PITOT. REMOVED & BLEW OUT DEBRIS. PERFORMED ADIR 1, ADIR 2, FCC 1, FCC SDR DALA2017032902519Light · out of adjustLT AFT EMERGENCY LIGHT INOPERATIVE. ADJUSTED LT AFT EXTERIOR EMERGENCY LIGHT PER B717 AMM 35-54. CHECKS OK.SDR DALA2017032902518Cusp Web · crackedCRACK ON RT CUSP WEB STA Y=218 X=-45 (CPAX). DAMAGE WAS REPAIRED PER SRM 53-00-55 FIG 221 REPAIR 4, HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND ALONG TRIM LINE PER NDT SPM 06-10-01.001.SDR DALA2017032802517Charger · inoperativeON SVC FOUND EMERG BATT PACK INOPERATIVE. R&R BATT CHARGER / BATT B5-235 REF AMM 33-51, WDM 33-51. CHECKS GOOD. OK FOR SVC.SDR DALA2017032802516Cusp Web · corrodedCORROSION ON LT CUSP WEB STA Y=549 BTW X=40 TO X=60. HFEC WAS ACCOMPLISHED ON LT CUSP WEB STA Y=549 BTW X=40 TO X=60, NO CRACKS WERE FOUND AFTER TRIM OUT PER NDT SPM 06-10-01.001. REPAIR WAS ACCOMPLISHED PER SRM 53-00-55 2R REPAIR 4. PERFORM DECAL CONDITION INSDR DALA2017032902555Skin · crackedSKIN CRACKED ON THE TOP OF THE FUSELAGE AT BS 1152 ON THE LEFT OF THE VERTICAL STAB. REPAIRED THE SKIN CRACK IAW ER/A 555585-14, AND PRI 555585-14, REV 0 AND 1.SDR DALA2017032802515Floor Support · corrodedCORROSION ON FLOOR SUPPORT FROM STA Y=130 TO Y= 148 X=-51 APPROX A COCKPIT. SUPPORT WAS REPLACED PER DWG 9936533 REV CM AND SRM 51-41-05 AND SRM 51-41-02.SDR DALA2017040502746Cusp Web · corrodedCORROSION ON CUSP WEB TOP SIDE BETWEEN ST 927-908 LBL 59. BLENDED CORROSION ON CUSP WEB TOPSIDE STA 908-927 LBL 59 WEB FOUND TO BE OUT OF LIMITS ORIGINAL THICKNESS .020" REMAINING .011" REMOVED .009" IAW SRM 53-00-55-1A-1 REPAIRED WEB BY INSTALLING DOUBLER IAWSDR DALA2017032702411Cusp Web · corrodedCORROSION ON LOWER SURFACE OF LEFT OTBD CUSP WEB LIGHTNING HOLE, BS 545 AND 551. BLENDED CORROSION IAW SRM 53-00-00-1A AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-55-1A-1. REPAIRED THE CUSP WEB IAW SRM 53-00-55-2R-4.SDR DALA2017032702410Cusp Web · corrodedCORROSION ON LOWER SURFACE OF LT OTBD CUSP WEB LIGHTNING HOLE AT BS 494. FOUND TO BE OUT OF LIMITS. FABRICATED A DOUBLER. TREATED, PRIMED, AND INSTALLED THE DOUBLER IAW SRM 53-00-55-2R-4, FIG 215, 4 C & D, 51-40-02, AND 51-10-04, PG 24, PAR 21, PG 16, PASDR DALA2017032702409Cusp Web · corrodedCORROSION ON LT CUSP WEB BS 530, LBL 40 - 60. REPAIRED IAW SRM 53-00-55 2R.SDR DALA2017032602407Pan · crackedCRACK ON RING PAN BS 636. THE PAN WAS REPAIRED IAW SRM 56-20-02-2R.,SDR DALA2017032602406Pan · crackedCRACK ON RING PAN , BS 756 AND 775. RING PAN WAS REPAIRED IAW SRM 56-20-02-2R.SDR DALA2017032902554Frame · corrodedCORROSION FRAME BS 946 BETWEEN LONGERONS 29 - 30R. REPAIRED IAW SRM 53-00-06-2R-2, AND 51-32-01.SDR DALA2017032702412Seat Track · damagedSEAT TRACK BS 200 - 256, RBL 44.5, GOUGED AND CORRODED. REMOVED CORROSION AND FOUND OUT OF LIMITS. REPLACED THE SEAT TRACK IAW SRM 53-20-52-1A-1, FIG 201, SRM 51-40-02-0G, 51-40-04, 51-41-08-0G, AND 51-41-05-0G.SDR DALA2017032502405Angle · corrodedR1 DOOR FRAME LOWER TRIANGLE POCKETS HAVE CORROSION. REPLACED RIGHT CUSP ANGLE FROM BS 158 TO 229 IAW SRM 53-00-55, REPAIR 3, SRM 51-41-02, & SRM 51-41-05.SDR DALA2017032902558Vane · delaminatedRIGHT FORWARD MOVEABLE VANE HAS DELAMINATION ON THE UPPER SKIN. REPAIRED THE VANE IAW SRM 57-53-01-2R-1, AND SRM 51-70-02-0G. RESTORED FINISH IAW AMM 51-10-00 370-805.SDR DALA2017032902556Skin · delaminatedRIGHT FORWARD MOVEABLE VANE HAS DELAMINATION ON THE UPPER SKIN. REMOVED FWD VANE, REPAIRED THE DELAMINATED AREA WITH A DOUBLER IAW SRM 57-53-01-2R-1, PARA 4B-4C, AND SRM 51-70-07-0G. INSTALLED THE VANE IAW AMM 27-50-03 400-801.SDR DALA2017032802514Skin · crackedSTA 1022 ABOVE LONGERON 14L FUSELAGE SKIN CRACKED AT FORMER LWR FWD FASTENER (EXTERNAL). HFEC VERIFIED IAW NDT SPM 06-10-01-.001 ETHF PROCEDURE 1, CUT OUT REGION OF EXTERNAL SKIN AND INTERNAL DOUBLER AND INSTALLED REPAIR AT FS 1022 ABOVE LONGERON 14L IAW ER/ASDR DALA2017032402374Door · dentedAPU DOOR HAS DENTS INCURRENCE PER TOPP 40-60-05, PARAGRAPH XBZ THAT THIS CONDITION IS ACCEPTABLE FOR A SINGLE NON-REVENUE FERRY FLIGHT FROM SLC TO VQQ PROVIDED LEFT HAND APU DOOR IS CLOSED. REPLACED LEFT APU ACCESS DOOR IAW SRM 51-41-01 AND DRAWING 5915081 REVSDR DALA2017032702413Attach Angle · chafedATTACH FLANGE UNDER PANEL 370AL CHAFED. THE ATTACH ANGLE WAS FOUND TO BE CRACKED, REPLACED THE ATTACH FLANGE IAW DWG 5910242, AND SRM 51-41-02.SDR DALA2017032302373Former · crackedLT CANTED KEEL FORMERS ARE CRACKED O/B ENDS STA 674, 696, 715. REPAIRED LT CANTED KEEL FORMERS IAW ER/A 545683-14MA REV 0.SDR DALA2017032202286Power Supply · inoperativeCABIN CEILING EMERGENCY LIGHTS ARE OUT. REPLACED THE POWER SUPPLY AND OPS CHECKED NORMAL IAW AMM 33-51.SDR DALA2017032202327Splice · corrodedCORROSION ON RT SIDE CUSP WEB AT FUSELAGE SKIN SPLICE BETWEEN FRAME STA 579-598 BELOW FLOOR. FOUND CORROSION TO BE ON CUSP ANGLE SPLICE ONLY. REPLACE CUSP ANGLE SPLICE IAW DWG 9910151 AND SRM 51-40-02.
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